What was found
FUSELAGE SKIN BULGING AND CRACKED BETWEEN 2 FASTENERS AT FS 1447.0, BETWEEN LONGERONS 30R AND 29R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00386 REV IR, DWG NR D85300386-001-D, REV IR, AND SRM CHAPTERS 51 & 53. HFEC OF REPAIR PARTS AND DAMAGE CUT-OUT AREA ON FUSELAGE ACCOMPLISHED IAW STEPS 4 AND 7 OF LISTED EVA, IAW NDT MANUAL. NO CRACKS OR CORROSION NOTED. FAA FORM 8110-3 ISSUED, DESIGNATION NR DERT-405157-CE, DATED 02DEC2010, FOR REPAIR DESIGN APPROVAL.